[1] |
ZHANG Junrui, ZHENG Xitao, YUAN Lin, ZHONG Guiyong, LI Guochen.
Fatigue life prediction method for hybrid multi-bolted joints based on damage weight
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524306-524306.
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[2] |
LI Zhenghong, XU Wu, ZHANG Xiaojing, YU Yin.
Experimental and analytical analyses of fatigue crack growth in sheets with multiple holes and cracks
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(7): 221867-221867.
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[3] |
CUI Ronghong, LIU Kai, HOU Bo, TAN Xiangfei, HE Yuting.
Crack monitoring based on high durability film sensor in coupled environment
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(3): 421535-421535.
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[4] |
CHAI Guozhong, LYU Jun, BAO Yumei, JIANG Xianfeng, DING Hao.
A highly efficient and accurate numerical analysis method for fatigue propagation of surface crack and life prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(12): 221291-221291.
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[5] |
ZHANG Fuze.
Theory and method of determination life by life factor
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(2): 404-410.
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[6] |
LIU Jianming, WAN Xiaopeng, ZHAO Meiying.
Fatigue life prediction of laminated bolted joint structures
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 1867-1875.
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[7] |
HONG Zhiliang, GAO Ge, JING Xiaodong, SUN Xiaofeng.
A grid-less time domain method for plate trailing edge noise prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(11): 3501-3514.
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[8] |
HOU Bo, HE Yuting, CUI Ronghong, ZHANG Teng, GAO Chao.
Crack Monitoring of Aircraft Metallic Structures Based on Ti/TiN Film Sensors
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(3): 878-884.
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[9] |
ZHANG Fuze.
Heavy Spectra Under Operational Loads May Reduce Life But Not Fatigue Scatter Factor
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(8): 1892-1897.
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[10] |
REN Jilin, CHEN Xi, LUO Shengcai, ZHOU Pei, LIU Changkui.
Research of High-cycle Fatigue Damage by Two-dimensional Magnetic Memory Testing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, (6): 1147-1155.
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[11] |
ZHANG Lishuang, WANG Tongqing, YANG Bing, ZHANG Wei.
Numerical Simulation of Sound Propagation from Varying Cross-section Ducts by Fast Scattering Method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(1): 62-67.
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[12] |
Wang Shengnan;Zheng Xiaoling.
Study on Proposed Rules to Preclude Widespread Fatigue Damage for Transport Category Aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(9): 1758-1768.
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[13] |
DU Lin;WANG Xiao-yu;SUN Xiao-feng.
A New Approach for the Acoustic Design of Aeroengine Nacelle
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1068-1072.
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[14] |
WANG Xiao-yu;DU Lin;SUN Xiao-feng.
A New Approach for the Acoustic Design of Aeroengine Nacelle with the Effect of Varying Cross-section Aera
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1073-1079.
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[15] |
YANG Xiao-hua;YAO Wei-xing;DUAN Cheng-mei.
Research on Fatigue Damage Cumulative Rule under Corrosion Environment
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(3): 234-236.
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